With objective of formulating realistic computing program to analyze panel flutter to aerospace vehicles, plausible simplifying assumptions are examined in light of experimental results; it is shown that in certain areas very simple analysis yields respectable results, whereas in other areas great elaboration is necessary to obtain accurate prediction; examples show that boundary layer greatly stabilizes flat plates in transonic or low supersonic flow and circular cylindrical shells at higher Mach numbers; recent contributions to panel flutter research at California Inst of Technology are summarized.


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    Titel :

    Some recent contribution to panel flutter research


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Fung, Y.C. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 4


    Erscheinungsdatum :

    1963


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Contribution to the Study of ''Panel Flutter''

    R. Barboni / P. Santini | NTIS | 1966


    Research on Panel Flutter

    Kobett, D. R. / Zeydel, E. F. E. | NTRS | 1963


    Research on panel flutter

    Kobett, D. R. | TIBKAT | 1964


    Some aspects of cylindrical shell panel flutter

    CARTER, L. / STEARMAN, R. | AIAA | 1967